# Service difficulty reports: N877FD

A list on [N877FD](https://openairdocs.org/aircraft/N877FD.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR FDEA202602060140](https://openairdocs.org/sdr/FDEA202602060140.md): Life Raft · miswired · Feb 6, 2026 · N877FD · Boeing 777F · Equipment/Furnishings Wiring
  > DURING RAFT INSPECTION FOUND CRES (SILVER) WIRE IS INSTALLED. NEED TO INSTALL COPPER WIRE. REMOVED L1 DOOR SLIDE, CUT INCORRECT SAFTEY WIRE FOR THE PACKBOARD RELEASE CABLE AND INSTALLED MS20995CY16 CAD-PLATED COPPER WIRE. REINSTALLED ORIGINAL L1 DOOR SL
- [SDR FDEA202601160059](https://openairdocs.org/sdr/FDEA202601160059.md): Floor Panel · cracked · Jan 16, 2026 · N877FD · Boeing 777F · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 242BF FOUND CRACKED. DAMAGE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A, ALLOWABLE DAMAGE 1, FIGURE 101-106, REV 51 & REPAIRED IAW SRM 53-00-50-2R, REPAIR 1, FIGURE 201-202, REV 51. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA202601160058](https://openairdocs.org/sdr/FDEA202601160058.md): Floor Panel · cracked · Jan 16, 2026 · N877FD · Boeing 777F · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 242LF FOUND CRACKED. DAMAGE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A, ALLOWABLE DAMAGE 1, FIGURE 101-106, REV 51 & REPAIRED IAW SRM 53-00-50-2R, REPAIR 1, FIGURE 201-202, REV 51. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA202601160057](https://openairdocs.org/sdr/FDEA202601160057.md): Floor Panel · cracked · Jan 16, 2026 · N877FD · Boeing 777F · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 241RF FOUND CRACKED. DAMAGE OUT OF ALLOWABLE LIMIT IAW SRM 53-00-50-1A, ALLOWABLE DAMAGE 1, FIGURE 101-106, REV 51 & REPAIRED IAW SRM 53-00-50-2R, REPAIR 1, FIGURE 201-202, REV 51. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA202601160056](https://openairdocs.org/sdr/FDEA202601160056.md): Floor Panel · cracked · Jan 16, 2026 · N877FD · Boeing 777F · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 241QF FOUND CRACKED. DAMAGE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A, ALLOWABLE DAMAGE 1, FIGURE 101-106, REV 51 & REPAIRED IAW SRM 53-00-50-2R, REPAIR 1, FIGURE 201-202, REV 51. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA202601160055](https://openairdocs.org/sdr/FDEA202601160055.md): Floor Panel · cracked · Jan 16, 2026 · N877FD · Boeing 777F · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 241LF FOUND CRACKED. DAMAGE OUT OF ALLOWABLE LIMIT IAW SRM 53-00-50-1A, ALLOWABLE DAMAGE 1, FIGURE 101-106, REV 51 & REPAIRED IAW SRM 53-00-50-2R, REPAIR 1, FIGURE 201-202, REV 51. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA202601160054](https://openairdocs.org/sdr/FDEA202601160054.md): Floor Panel · cracked · Jan 16, 2026 · N877FD · Boeing 777F · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 241PF FOUND CRACKED. DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A, ALLOWABLE DAMAGE 1, FIGURE 101-106, REV 51 & REPAIRED IAW SRM 53-00-50-2R, REPAIR 1, FIGURE 201-202, REV 51.. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA202601160053](https://openairdocs.org/sdr/FDEA202601160053.md): Floor Panel · cracked · Jan 16, 2026 · N877FD · Boeing 777F · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 241SF FOUND CRACKED. DAMAGE OUT OF ALLOWABLE LIMIT IAW SRM 53-00-50-1A, ALLOWABLE DAMAGE 1, FIGURE 101-106, REV 51 & REPAIRED IAW SRM 53-00-50-2R, REPAIR 1, FIGURE 201-202, REV 51. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA202601160052](https://openairdocs.org/sdr/FDEA202601160052.md): Floor Panel · cracked · Jan 16, 2026 · N877FD · Boeing 777F · Fuselage Floor Panel
  > MAIN DECK CARGO. FLOOR PANEL 241HF FOUND CRACKED. DAMAGE OUT OF ALLOWABLE LIMIT IAW SRM 53-00-50-1A, ALLOWABLE, DAMAGE 1, FIGURE 101-106, REV 51. & REPAIRED IAW SRM 53-00-50-2R, REPAIR 1, FIGURE 201-202, REV 51. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA202601160051](https://openairdocs.org/sdr/FDEA202601160051.md): Floor Panel · cracked · Jan 16, 2026 · N877FD · Boeing 777F · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 241JF FOUND CRACKED. DAMAGE OUT OF ALLOWABLE LIMIT IAW SRM 53-00-50-1A, ALLOWABLE DAMAGE 1, FIGURE 101-106, REV 51.0 AND REPAIRED IAW SRM 53-00-50-2R, REPAIR 1, FIGURE 201-202, REV 51. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA202601140030](https://openairdocs.org/sdr/FDEA202601140030.md): Skin · cracked · Jan 14, 2026 · N877FD · Boeing 777F · Wing, Plate/Skin
  > DURING PERFORMANCE OF WORK CARD:EG-5710-E0376285E P12 STEP 3.B. & STEP 5.A.(2), FOUND ONE CRACK ON THE RT UPPER WING SKIN FASTENER NR 5. REPAIRED IAW SRM 51-40-05-0G FIGURE 4 TABLE C, SRM 51-40-02-0G FIGURE 12, SRM 51-40-04-0G FIGURE 2 TABLE A, REV 51.0
- [SDR FDEA202601140029](https://openairdocs.org/sdr/FDEA202601140029.md): Skin · cracked · Jan 14, 2026 · N877FD · Boeing 777F · Wing, Plate/Skin
  > DURING PERFORM WORK CARD:EG-5710-E0376285E P11 STEP 3.B.& STEP 5.A.(2) THEN FOUND TWO CRACKS ON THE LT UPPER WING SKIN FASTENER 5. REPAIRED IAW SRM 51-40-05-0G FIGURE 4 TABLE C, SRM 51-40-02-0G FIGURE 12, SRM 51-40-04-0G FIGURE 2 TABLE A, REV 51.0 AND EA G
- [SDR FDEA202309211631](https://openairdocs.org/sdr/FDEA202309211631.md): Lamp · failed · Sep 21, 2023 · N877FD · Boeing 777FS2 · Emergency Lighting
  > POST-FLT INSP, SUPRNMRY EMERGENCY LT INOP IN GALLEY DIRECT OVERHEAD CEILING. AMM: 33-51-04-2 RE-LAMPED, REF B777 AMM: 33-51-04-2. LT'S TEST SATIS, ITEM OK FOR SVC.
- [SDR FDEA202305090833](https://openairdocs.org/sdr/FDEA202305090833.md): Floor Panel · cracked · May 9, 2023 · N877FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 242QF(PN:152W8652-4) AT STA1451-1452.25/RBL44 FOUND CRACK.(OFF WING). MAIN DECK CARGO FLOOR PANEL 242QF (PN:152W8652-4) AT STA 1451-1452.25/RBL44 CRACK (OFF WING),DAMAGE SIZE:L=1.3" IN LOWER SKIN WITHIN LIMIT. EVALUATED THE DAM
- [SDR FDEA202305090832](https://openairdocs.org/sdr/FDEA202305090832.md): Floor Panel · cracked · May 9, 2023 · N877FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 242PF(PN:152W8652-6) AT STA1473.75/RBL83-84 FOUND CRACK. (OFF WING). MAIN DECK CARGO FLOOR PANEL 242PF (PN:152W8652-6) AT STA 1473.75/RBL 83-84 CRACK (OFF WING), DAMAGE SIZE:L=1" IN LOWER SKIN WITHIN LIMIT. EVALUATED THE DAMAGE
- [SDR FDEA202305090831](https://openairdocs.org/sdr/FDEA202305090831.md): Floor Panel · cracked · May 9, 2023 · N877FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 241UF(PN:152W8652-3) AT STA1446-1447/LBL73.75-75.75 FOUND CRACK.(OFF WING). MAIN DECK CARGO FLOOR PANEL 241UF(PN:152W8652-3) AT STA1446-1447/LBL73.75-75.75 CRACK (OFF WING),DAMAGE SIZE:L=2" IN LOWER SKIN WITHIN LIMIT. EVALUATED
- [SDR FDEA202305090830](https://openairdocs.org/sdr/FDEA202305090830.md): Floor Panel · cracked · May 9, 2023 · N877FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 241QF(PN:152W8452-21) AT STA1358/LBL52-54.75 FOUND CRACK. (OFF WING). MAIN DECK CARGO FLOOR PANEL 241QF(PN:152W8452-21) AT STA1358/LBL52-54.75 CRACK (OFF WING). DAMAGE SIZE:L=2.75" IN LOWER SKIN WITHIN LIMIT. EVALUATED THE DAMAG
- [SDR FDEA202305090829](https://openairdocs.org/sdr/FDEA202305090829.md): Floor Panel · cracked · May 9, 2023 · N877FD · Boeing 777FS2 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 241PF(PN:152W8452-19) AT STA1309.5-1310/LBL20-22 FOUND CRACK(OFF WING). MAIN DECK CARGO FLOOR PANEL 241PF(PN:152W8452-19) AT STA1309.5-1310/LBL20-22 CRACK(OFF WING).DAMAGE SIZE:L=2.1" IN LOWER SKIN WITHIN LIMIT. EVALUATED AND
- [SDR FDEA202011142848](https://openairdocs.org/sdr/FDEA202011142848.md): Lamp · inoperative · Nov 14, 2020 · N877FD · Boeing 777 · Emergency Lighting
  > 1 OVERHEAD EMERGENCY EXIT LIGHT IS INOPERATIVE IN THE SUPERNUMERARY AREA. RELAMPED CEILING AREA EMERGENCY LIGHT, REF 777 AMM 33-51-03-2. OPERATIONS CHECK GOOD. A/C OK FOR SERVICE.
- [SDR FDEA202011142847](https://openairdocs.org/sdr/FDEA202011142847.md): Lamp · inoperative · Nov 14, 2020 · N877FD · Boeing 777 · Emergency Lighting
  > 1 OVERHEAD EMERGENCY EXIT LIGHT IS INOPERATIVE IN THE SUPERNUMERARY AREA. RELAMPED CEILING AREA EMERGENCY LIGHT, REF 777 AMM 33-51-03-2. OPERATIONS CHECK GOOD. A/C OK FOR SERVICE. LAMP P/N P78749-001.
- [SDR FDEA202008272045](https://openairdocs.org/sdr/FDEA202008272045.md): Lamp · inoperative · Aug 27, 2020 · N877FD · Boeing 777F · Emergency Lighting
  > CEILING EMERGENCY LIGHT IS OUT IN COURIER CABIN. RE-LAMPED, REF B777 AMM: 33-51-03-2. EMERGENCY LIGHTS TEST SATISFACTORY, ITEM OK FOR SERVICE.
- [SDR FDEA201806141491](https://openairdocs.org/sdr/FDEA201806141491.md): Power Supply · inoperative · Jun 14, 2018 · N877FD · Boeing 777FS2 · Emergency Lighting
  > DURING PREFLIGHT OF SUPERNUMERARY AREA FOUND 2 EMERGENCY EXIT LIGHT INOP. R&R L1 POWER SUPPLE "M33093". P/N D717-02-001. S/N 157327. CHECKS OK REF MM 33-51-06-2. OK TO CONT.

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N877FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N877FD/reports

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